分类
_笔记_

MST Method

1 前言

MST method 是由 Mano, Suzuki, and Takasugi $($MST$)$ [1]建立的一种得到一些较特殊的微分方程的解析解的一种方法。这种方法最初是为了解决Teukolsky equation[2]而建立的。

在此之前,已有一些求解 Teukolsky equation 解析解的相关工作[3]-[5]。尤其强调的是Leaver[5]做了一些系统性的工作。

考虑到写这篇笔记的目的是:记录在复算相关论文时遇到的障碍以及解决的过程,从而希望整理出MST method的较为详细且通顺的逻辑。于是就不再强调过多的背景内容。

考虑到笔者能力有限,可能会在一些细节上理解不透彻甚至有误。希望读者多多包涵并联系我们指出不足之处^ω^。

2 内容

这里以解决GMGHS时空下无质量的标量波被散射的问题[6]为背景,来介绍MST method 的应用。

Klein-Gordon Equation:

$$ \nabla_\mu\nabla^\mu\Phi=0 $$

对其分离变量后会得到一个较为复杂的径向方程:$$\Delta\frac{d}{dr}\left(\Delta\frac{dR_{\omega l}}{dr}\right)+\left[G(r)^2\omega^2r^4-\Delta l(l+1)\right]R_{\omega l}=0$$
其中
$G(r) = 1-\frac{Q^2}{Mr}$
$\Delta=\left(r-r_+\right)\left(r-r_-\right)$
$r_+=2M$ , $r_-=2Mq^2$

这里我们不过多关注方程中参数的具体含义。论文[6]在视界$r_{+}$附近和无穷远处,分别得到了两个有各自收敛范围的解析解。两种解的获取方法是类似的,这里以较为复杂的无穷远处的情况为例来讲解。

对径向方程中的变量做线性变换并使其无量纲化:
$$x=-\frac{r-r_+}{\kappa r_+};\kappa=1-\frac{Q^2}{2M^2};\epsilon=2M\omega$$
方程变为
$$x(1-x)\frac{d^2 R}{d x^2}+(1-2x)\frac{d R}{d x}+UR=0$$
其中
$$U=\frac{\epsilon^2}{x}+l(l+1)-(1+2\kappa)\epsilon^2+(2+\kappa)\kappa\epsilon^2 x-\kappa^2\epsilon^2 x^2$$

(最近有点忙,有空慢慢写)



引用

[1] arXiv:gr-qc/9603020v3 19 Mar 1996
[2] S.A.Teukolsky,Astorophys.J.185,635(1973).
[3] D.N.Page,Phys.Rev.D13,198(1976).
[4] A.A.StarobinskyandChurilov,Sov.Phys.JETP38,1(1974).
[5] E.W.Leaver,J.Math.Phys.27,1238(1986).
[6] Eur. Phys. J. C (2020) 80:654

分类
_笔记_ 简介 粒子物理

基本粒子简介

本文是格里菲斯大神Introduction to Elementary Particles一书简介部分的笔记

物质是如何构成的
分类
_笔记_ 广义相对论 张量分析

牛顿力学下的潮汐效应

本文适合作为张量分析自学入门的一个案例

从牛顿引力和运动学公式出发,利用张量语言推到和描述经典力学框架下的潮汐效应,张量分析的初学者可以此为例联系基本计算和对方向导数的理解,同时作为广义相对论中测地线偏离理论的先导

Newton’s second law (componentwise)

$$
\frac{d^{2} x^{i}}{d t^{2}} \equiv a^{i} \equiv \frac{F^{i}}{m}
$$

Newtonian equation of gravitation

$$
\frac{F^{i}}{m}=-\eta^{i j} \partial_{j} \phi
$$

combine two equations give:

$$
\frac{d^{2} x^{i}}{d t^{2}}=-\eta i j\left[\partial_{j} \phi\right]_{\vec{x}}
$$

where the subscription $\vec{x}$ denotes the derivative is operated at position $\vec{x}$ similarly we have at $\vec{x}+\vec{n}$ :

$$
\frac{d^{2}\left(x^{i}+n^{i}\right)}{d t^{2}}=-\eta^{i j}\left[\partial_{j} \phi\right]_{\vec{x}+\vec{n}}
$$

make subtraction give:

$$
\frac{d^{2} n^{i}}{d t^{2}}=-\eta^{i j}\left(\left[\partial_{j} \phi\right]{\vec{x}+\vec{n}}-\left[\partial{j} \phi\right]_{\vec{x}}\right)
$$

given $\vec{n}$ is infinitesimal, we have RHS:

$$
\text { RHS }=-\eta^{i j} n^{k}\left[\partial_{k}\left(\partial_{j} \phi\right)\right]_{\vec{x}}
$$

set Cartesian coordinates originated from centre of earth orient the $z$-axis so that is consists with $\vec{x}$ (position vector) then $\vec{X}=\left(X^{1}, X^{2}, X^{3}\right)=(0,0, z)$.

gravitational potential is given by:

$$
\phi=-\frac{G M}{r}=-\frac{G M}{\left(x^{2}+y^{2}+z^{2}\right)^{1 / 2}}
$$

and thus

$$
\begin{aligned}
\partial_{j} \phi & =\frac{\partial \phi}{\partial x^{j}} \\
& =-\frac{d \phi}{d r} \frac{\partial r}{\partial x^{j}} \\
& =\frac{G M}{r^{3}} x^{j}
\end{aligned}
$$

and

$$
\begin{aligned}
\partial_{k} \partial_{j} \phi & =\frac{\partial}{\partial x^{k}}\left(\frac{G M}{r^{3}} x^{j}\right) \\
& =\frac{\partial}{\partial x^{k}}\left(\frac{G M}{r^{3}}\right) x^{j}+\delta_{k}^{j} \frac{G M}{r^{3}} \\
& =-\frac{3 G M}{r^{4}} x^{j}+\delta_{k}^{j} \frac{G M}{r^{3}}
\end{aligned}
$$

thus.
$$
\begin{aligned}
& \frac{d^{2}}{d t^{2}} n^{x}=-\frac{G M}{r^{3}} n^{x} \\
& \frac{d^{2}}{d t^{2}} n^{y}=-\frac{G M}{r^{3}} n^{y} \\
& \frac{d^{2}}{d t^{2}} n^{z}=\frac{2 G M}{r^{3}} n^{z}
\end{aligned}
$$

分类
_笔记_ 分析力学

由拉格朗日方程导出欧拉动力学方程

本文整理自俞千野同学的工作,预备役物理民工经授权搬运

千野哥哥太强了

Lagrangian of free rigid body in its comoving reference frame is given by:

$$
L=\sum_{i} \frac{1}{2} I_{i} \omega_{i}^{2}
$$

where angular velocities can be expressed in Eulerian angles: $\omega_{1}=\dot{\varphi} \sin \theta \sin \psi+$ $\dot{\theta} \cos \psi, \omega_{2}=\dot{\varphi} \sin \theta \cos \psi-\dot{\theta} \sin \psi, \omega_{3}=\dot{\varphi} \cos \theta+\dot{\psi}$.

Substitute into EL equations:

$$
\frac{d}{d t}\left(\frac{\partial \mathcal{L}}{\partial \dot{q}_{i}}\right)=\frac{\partial \mathcal{L}}{\partial q_{i}}
$$

where $q_{i}$ take $q_{1}=\theta, q_{2}=\varphi, q_{3}=\psi$.

Apply chain rule to both sides of (2) :

$$
\begin{aligned}
\frac{\partial \mathcal{L}}{\partial q_{i}} & =\sum_{j=1}^{3} \frac{\partial \mathcal{L}}{\partial \omega_{j}} \frac{\partial \omega_{j}}{\partial q_{i}} \\
\frac{\partial \mathcal{L}}{\partial \dot{q}_{i}} & =\sum_{j=1}^{3} \frac{\partial \mathcal{L}}{\partial \omega_{j}} \frac{\partial \omega_{j}}{\partial \dot{q}_{i}}
\end{aligned}
$$

Substitute $q_{3}$ by $\psi$ in (2), RHS:

$$
\begin{aligned}
\frac{\partial \mathcal{L}}{\partial \psi} & =\sum_{i=1}^{3} \frac{\partial \mathcal{L}}{\partial \omega_{i}} \frac{\partial \omega_{i}}{\partial \psi} \\
& =\sum_{i=1}^{3} I_{i} \omega_{i} \frac{\partial \omega_{i}}{\partial \psi} \\
& =I_{1} \omega_{1}(\dot{\varphi} \sin \theta \cos \psi-\dot{\theta} \sin \psi)+I_{2} \omega_{2}(-\dot{\varphi} \sin \theta \sin \psi-\dot{\theta} \cos \psi)+0 \\
& =I_{1} \omega_{1} \omega_{2}+I_{2} \omega_{2}\left(-\omega_{1}\right) \\
& =\left(I_{1}-I_{2}\right) \omega_{1} \omega_{2}
\end{aligned}
$$

*this note is rearranged based on Qianye YU’s work LHS:

$$
\frac{d}{d t}\left(\frac{\partial \mathcal{L}}{\partial \dot{\psi}}\right)=I_{3} \dot{\omega}_{3}
$$

Combing (2)(4)(5) gives the first Euler dynamic equation:

$$
\left(I_{1}-I_{2}\right) \omega_{1} \omega_{2}-I_{3} \dot{\omega}_{3}=0
$$

Similarly substitute $q_{2}$ by $\varphi$ into equation(2). Since $\frac{\partial \mathcal{L}}{\partial \varphi}=0$, we have:

$$
\frac{d}{d t}\left(\frac{\partial \mathcal{L}}{\partial \dot{\varphi}}\right)=0
$$

Apply chain rule to LHS of (7) gives:

$$
\begin{aligned}
0= & I_{1} \dot{\omega}_{1} \sin \theta \sin \psi+I_{2} \dot{\omega}_{2} \sin \theta \cos \psi+I_{3} \dot{\omega}_{3} \cos \theta+I_{1} \omega_{1}(\cos \theta \sin \psi \dot{\theta} \\
& +\sin \theta \cos \psi \dot{\psi})+I_{2} \omega_{2}(\cos \theta \cos \psi \dot{\theta}-\sin \theta \sin \psi \dot{\psi})-I_{3} \omega_{3} \sin \theta \dot{\theta}
\end{aligned}
$$

We introduce $A=I_{1} \omega_{1}(\cos \theta \sin \psi \dot{\theta}+\sin \theta \cos \psi \dot{\psi})$ and $B=I_{2} \omega_{2}(\cos \theta \cos \psi \dot{\theta}-$ $\sin \theta \sin \psi \dot{\psi})$ to reduce the calculation.

Notice $I_{3} \dot{\omega}_{3}=\left(I_{1}-I_{2}\right) \omega_{1} \omega_{2}$. So (8) is equivalent to:

$$
\begin{aligned}
\sin \theta\left[I_{1} \dot{\omega}_{1} \sin \psi+I_{2} \dot{\omega}_{2} \cos \psi\right] & =\left(I_{2}-I_{1}\right) \omega_{1} \omega_{2} \cos \theta+I_{3} \omega_{3} \sin \theta \dot{\theta}-A-B \\
& =I_{1}\left(-\omega_{1} \omega_{2} \cos \theta-\omega_{1} \cos \theta \sin \psi \dot{\theta}-\omega_{1} \sin \theta \cos \psi \dot{\psi}\right) \\
& +I_{2}\left(\omega_{1} \omega_{2} \cos \theta-\omega_{2} \cos \theta \cos \psi \dot{\theta}+\omega_{2} \sin \theta \sin \psi \dot{\psi}\right) \\
& +I_{3} \omega_{3} \sin \theta \dot{\theta} \\
& =I_{1} \omega_{1}(-\dot{\varphi} \sin \theta \cos \psi \cos \theta+\dot{\theta} \sin \psi \cos \theta-\dot{\theta} \sin \psi \cos \theta\\&-\sin \theta \cos \psi \dot{\psi})  +I_{2} \omega_{2}(\dot{\varphi} \sin \theta \sin \psi \cos \theta+\dot{\theta} \cos \psi \cos \theta\\&-\dot{\theta} \cos \psi \cos \theta+\sin \theta \sin \psi \dot{\psi})  +I_{3} \omega_{3} \sin \theta \dot{\theta} \\
& =I_{1} \omega_{1}(-\dot{\varphi} \sin \theta \cos \psi \cos \theta-\sin \theta \cos \psi \dot{\psi}) \\
& +I_{2} \omega_{2}(\dot{\varphi} \sin \theta \sin \psi \cos \theta+\sin \theta \sin \psi \dot{\psi}) \\
& +I_{3} \omega_{3} \sin \theta \dot{\theta}
\end{aligned}
$$

Dividing (9) through $\sin \theta$ gives:

$$
\begin{aligned}
I_{1} \dot{\omega}_{1} \sin \psi+I_{2} \dot{\omega}_{2} \cos \psi & =I_{1} \omega_{1}(-\dot{\varphi} \cos \psi \cos \theta-\cos \psi \dot{\psi}) \\
& +I_{2} \omega_{2}(\dot{\varphi} \sin \psi \cos \theta+\sin \psi \dot{\psi}) \\
& +I_{3} \omega_{3} \dot{\theta}
\end{aligned}
$$

We keep equation (10) for later use

Substituting $q_{3}$ by $\theta$ into equation $(2)$ :

$$
\frac{d}{d t}\left(\frac{\partial \mathcal{L}}{\partial \dot{\theta}}\right)=\frac{\partial \mathcal{L}}{\partial \theta}
$$

So,

$$
\begin{aligned}
\frac{d}{d t}\left(I_{1} \omega_{1} \cos \psi-I_{2} \omega_{2} \sin \psi\right)= & I_{1} \omega_{1} \dot{\varphi} \cos \theta \sin \psi+I_{2} \omega_{2} \dot{\varphi} \cos \theta \cos \psi \\
& +I_{3} \omega_{3} \dot{\varphi}(-\sin \theta)
\end{aligned}
$$

which gives:

$$
\begin{aligned}
I_{1} \dot{\omega}_{1} \cos \psi-I_{2} \dot{\omega}_{2} \sin \psi= & I_{1} \omega_{1}(\dot{\varphi} \cos \theta \sin \psi+\sin \psi \dot{\psi}) \\
& +I_{2} \omega_{2}(\dot{\varphi} \cos \theta \cos \psi+\cos \psi \dot{\psi}) \\
& -I_{3} \omega_{3} \dot{\varphi} \sin \theta
\end{aligned}
$$

Since (10) and (13) are obtained from EL equation of generalized coordinates $\varphi$ and $\theta$ respectively, along with (6), we have used all three independent EL equations, the other two Euler equations must be obtained directly from combinations of (10) and (13):

Firstly, (10) $\cdot \sin \psi+(13) \cdot \cos \psi$ gives:

$$
\begin{aligned}
I_{1} \dot{\omega}_{1} & =I_{2} \omega_{2}(\dot{\varphi} \cos \theta+\dot{\psi})+I_{3} \omega_{3}(\dot{\theta} \sin \psi-\dot{\varphi} \sin \theta \cos \psi) \\
& =I_{2} \omega_{2} \omega_{3}+I_{3} \omega_{3}\left(-\omega_{2}\right) \\
& =\left(I_{2}-I_{3}\right) \omega_{2} \omega_{3}
\end{aligned}
$$

And $(10) \cdot \cos \psi-(13) \cdot \sin \psi$ gives:

$$
\begin{aligned}
I_{2} \dot{\omega}_{2} & =I_{1} \omega_{1}(-\dot{\varphi} \cos \theta-\dot{\psi})+I_{3} \omega_{3}(\dot{\theta} \cos \psi+\dot{\varphi} \sin \theta \sin \psi) \\
& =I_{1} \omega_{1}\left(-\omega_{3}\right)+I_{3} \omega_{3} \omega_{1} \\
& =\left(I_{3}-I_{1}\right) \omega_{3} \omega_{1}
\end{aligned}
$$

Rearranging (6),(14),(15) gives the Eulerian dynamic equations:

$$
\left\{\begin{array}{l}
\left(I_{1}-I_{2}\right) \omega_{1} \omega_{2}-I_{3} \dot{\omega}_{3}=0 \\
\left(I_{2}-I_{3}\right) \omega_{2} \omega_{3}-I_{1} \dot{\omega}_{1}=0 \\
\left(I_{3}-I_{1}\right) \omega_{3} \omega_{1}-I_{2} \dot{\omega}_{2}=0
\end{array}\right.
$$

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